US3435893A - Heat exchanger component formed with flexible plastic tubes - Google Patents
Heat exchanger component formed with flexible plastic tubes Download PDFInfo
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- US3435893A US3435893A US3435893DA US3435893A US 3435893 A US3435893 A US 3435893A US 3435893D A US3435893D A US 3435893DA US 3435893 A US3435893 A US 3435893A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C57/00—Shaping of tube ends, e.g. flanging, belling or closing; Apparatus therefor, e.g. collapsible mandrels
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
- B23P15/26—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass heat exchangers or the like
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/18—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/18—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools
- B29C65/24—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools characterised by the means for heating the tool
- B29C65/30—Electrical means
- B29C65/305—Electrical means involving the use of cartridge heaters
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/34—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
- B29C65/3404—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the type of heated elements which remain in the joint
- B29C65/3408—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the type of heated elements which remain in the joint comprising single particles, e.g. fillers or discontinuous fibre-reinforcements
- B29C65/3412—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the type of heated elements which remain in the joint comprising single particles, e.g. fillers or discontinuous fibre-reinforcements comprising fillers
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/34—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
- B29C65/3472—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the composition of the heated elements which remain in the joint
- B29C65/3484—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the composition of the heated elements which remain in the joint being non-metallic
- B29C65/3492—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement" characterised by the composition of the heated elements which remain in the joint being non-metallic being carbon
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/13—Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
- B29C66/137—Beaded-edge joints or bead seals
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/52—Joining tubular articles, bars or profiled elements
- B29C66/522—Joining tubular articles
- B29C66/5227—Joining tubular articles for forming multi-tubular articles by longitudinally joining elementary tubular articles wall-to-wall (e.g. joining the wall of a first tubular article to the wall of a second tubular article) or for forming multilayer tubular articles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/83—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
- B29C66/832—Reciprocating joining or pressing tools
- B29C66/8322—Joining or pressing tools reciprocating along one axis
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C67/00—Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00
- B29C67/0044—Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00 for shaping edges or extremities
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F21/00—Constructions of heat-exchange apparatus characterised by the selection of particular materials
- F28F21/06—Constructions of heat-exchange apparatus characterised by the selection of particular materials of plastics material
- F28F21/062—Constructions of heat-exchange apparatus characterised by the selection of particular materials of plastics material the heat-exchange apparatus employing tubular conduits
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
- F28F9/007—Auxiliary supports for elements
- F28F9/013—Auxiliary supports for elements for tubes or tube-assemblies
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2793/00—Shaping techniques involving a cutting or machining operation
- B29C2793/0027—Cutting off
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/52—Joining tubular articles, bars or profiled elements
- B29C66/522—Joining tubular articles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/725—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being hollow-walled or honeycombs
- B29C66/7252—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being hollow-walled or honeycombs hollow-walled
- B29C66/72523—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being hollow-walled or honeycombs hollow-walled multi-channelled or multi-tubular
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/18—Heat-exchangers or parts thereof
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/60—Multitubular or multicompartmented articles, e.g. honeycomb
- B29L2031/601—Multi-tubular articles, i.e. composed of a plurality of tubes
- B29L2031/602—Multi-tubular articles, i.e. composed of a plurality of tubes composed of several elementary tubular elements
Definitions
- An assemblable component suitable for heat exchange, or heat transfer comprising a plurality of elongated flexible plastic tubular elements arranged in a substantially flat laterally disposed single layer side-by-side array, said tubular elements of at least one portion of the component having their laterally adjacent portions physically united to each other to form a single integral molded structure extending transversely of said array, said molded structure having passageways of a particular transverse crosssection extending therethrough, each communicating with the interior of a tube element at at least one end of the molded structure, the molded structure having a particular configuration to permit stacking or windup to produce multi-layer units. Also involved is an improved manufacturing arrangement for producing the simplified easily assemblable components.
- This invention relates generally to heat exchange, or heat transfer, apparatus; and more specifically to a particular heat exchange apparatus construction formed from flexible plastic tube elements and especially useful in certain applications.
- the flexible plastic tube elements must be individually threaded through baifle members and secured individually in tube sheet members.
- the tube elements are fashioned into bundles using transverse tapes which must be secured to the tube elements by welding or adhesives.
- additional means such as foraminous cylinders, or baskets, are needed in addition to the tapes to maintain the position and size of a ⁇ bundle of heat exchange tubes.
- Bundles of flexible plastic tubes also have been formed by assembling sleeves of braided tubes in order to provide coherent stable bundles (application Ser. No. 634,631, filed Apr. 28, 1967).
- the components of this invention due to their simplicity, no additional elements being required, in the preferred version, other than the flexible plastic tube elements themselves, and due to the ease of assembly into composite heat exchanger units, presents an improved product over the prior art arrangements and also makes possible the use of more simple and eflicient production techniques.
- the improved component due to its novel construction, can be used to produce special configuration heat exchanger units greatly reduced in one of their three dimensions for use in special limited space applications.
- the elimination of tapes, and braids, and supporting baskets in the preferred embodiments of the invention not only reduces complexity and cost, but also improves fluid flow characteristics by reducing pressure drop and reducing susceptibility to clogging due to foreign matter in the fluid streams being handled exteriorly of the hollowtubular elements.
- the improved component when used in a flat warp configuration of the tube elements, or in a rectangular transverse crosssection multi-layer assembly is especially advantageous in heat exchangers of the cross flow type in which one fluid stream is passed substantially perpendicularly, or transversely, across a bundle of tube elements carrying another fluid stream for heat transfer between the streams.
- FIGURES 1A and 1B are perspective views of the main units of the apparatus for forming the improved component of this invention, by creating a tight enclosure around a warp of tube elements and applying the required heat and reduced pressure to the tube elements to physically unite them.
- FIGURE 2 is a partial perspective view of the terminal portions of a single layer parallel array of plastic tube elements positioned between two opposed heated surfaces as would occur in the units of FIGURES 1A and 1B to apply the heat and pressure to physically unite the tube elements to form the component of this invention.
- FIGURE 3 is a view similar to FIGURE 2 showing the united tube elements of the component of this invention.
- FIGURE 4 is a partial plan view of the apparatus unit of FIGURE 1B showing a warp or array of tube elements positioned therein prior to the uniting operation.
- FIGURE 5 is a general schematic showing of one overall arrangement for producing components suitable for heat exchange and embodying principles of the invention.
- FIGURE 6 is a perspective exploded view of a simplified heat exchange unit formed using a single component of this invention.
- FIGURE 7 is a partial perspective view of one end of a rectangular transverse cross-section heat exchanger unit formed by assembling a plurality of components of this invention.
- FIGURE 8 is a partial simplified perspective view of an overall cross flow heat exchanger utilizing a rectangular transverse cross-section assembly of components of this invention with certain parts broken away for a clearer general showing.
- FIGURE 9 is a series of schematic views. of components of the invention showing a number of the possible transverse cross-sectional arrangements of the united molded structure which would permit assembly by stacking or winding up of components.
- FIGURE is an exploded perspective view of an assembled heat exchange unit utilizing components of this invention Which have the transverse molded or united structure formed not only across the terminal portion of the tube elements to facilitate connection to the header members, but also across intermediate portions of the tube elements to provide for heat transfer between alternate layers of the tube elements without the need for the usual shell or casing.
- FIGURE 11 is a generalized schematic showing of another arrangement for producing components embodying principles of this invention and assembling the component into a multilayer bundle.
- FIGURES 12 and 13 show multilayer bundles of different transverse cross sections which can be prepared by the arrangement of FIGURE 11.
- FIGURE 3 The basic structure of an assemblable component embodying principles of the invention is shown in FIGURE 3.
- FIGURE 6 One version of a complete component embodying features of the invention is shown in FIGURE 6 and identified by the reference character HXCI.
- the component comprises a side- 'by-side single layer array or warp of elongated flexible tube elements T formed of an organic polymeric composition, which tube elements are laterally joined together or physically united in at least one transversely extending integral structure MS.
- the tube elements are united by any suitable means, preferably a molding arrangement to be described at a later point.
- This integral structure is provided with elongated passageways P extending therethrough, each passageway communicating with the interior of a hollow tubular element T at at least one end of the integral or molded structure MS.
- the passageways in the integral structure have generally uniform transverse cross sections. with four sides as shown.
- the opposed walls 10 which divide the integral structure laterally to form the passageways P are substantially parallel to each other and are generally planar. These Walls 10 are joined or connected as shown in FIGURE 3 by two opposed equidistant walls 11 which are faired together in a lateral direction to form opposing transversely extending regular surfaces constructed and arranged to engage and match with other similar structures of tubular elements, or with other portions of the same structure when folded or wound, so that a heat exchange bundle of a plurality of layers, as shown in FIGURES 7, 8, 10, ll, 12 and 13, can conveniently be assembled and formed.
- the preferred and simplest arrangement of fairing together the equidistant walls to provide the regular opposed surfaces suitable for forming multi-layer arrangements is the one in which all of the opposed walls on one side of the molded structure are joined to form a single transversely extending planar surface as shown in FIGURE 3.
- Other arrangements may be formed and used such as those having transverse cross sections as shown in FIGURE 9.
- the heat exchange bundles are formed by winding or stacking the assemblable components and suitably bonding these components together at least at the end portions where the tube elements are physically united to form the transversely extending integral molded structures.
- the component HXCI shown in FIGURE 6 can be provided with a relatively rigid supporting framework, which may be a wire grid interwoven with the tube elements T. As shown the grid comprises transversely extending elements 56 which are interconnected at their end portions by longitudinal elements 55.
- the supporting framework is used where it is desired to maintain the flexible array of tube elements in a given position and for configuration.
- FIGURE 8 Another type of supporting framework is shown in FIGURE 8 in which a tube bundle of rectangular transverse cross section is built up of a plurality of single layer arrays of tube elements or components of the invention.
- the framework of FIGURE 8 comprises at a number of longitudinally spaced positions along the bundle of tube elements, a plurality of transversely extending members 66 each placed between a layer of tube elements and joined at their ends by elongated bolt members 67. If desired, the transversely extending members 66 may be further secured in place by an adhesive bond to the engaged layers of tube elements.
- FIGURE 10 Another version of the assemblable component of the invention is disclosed in FIGURE 10. These components are identical with the components shown in FIGURES 3 and 6 except that they are further provided intermediate their end portions with an additional transversely extending integral molded structure MSA formed by physically united tube elements for a purpose to be disclosed hereinafter.
- the components embodying principles of the invention may be used individually as shown in FIGURE 6 by suitably securing and sealing the transversely extending molded structures MS in openings 52, 54 in header members 51 and 53 respectively.
- the component of course may be used with and without a supporting framework.
- Header members 51 and 53 can conveniently be made of an organis polymeric composition compatible with the material of which the tube elements are formed.
- the components of the invention may be used in a multilayer stacked arrangement as shown in FIGURES 7 and 8.
- This arrangement is formed by stacking or superimposing one on the other a plurality of components such as those shown in FIGURES 3 and 6 and sealing or bonding the transversely extending integral molded structures MS to each other at each end of the stacked arrangement.
- a bundle of tube elements with a rectangular transverse cross section is formed as seen in FIGURE 7.
- a rigidly secured peripherally surrounding flange member 59 is provided at each end of the bundle to assist in its assembly into a complete heat exchanger apparatus of the type generally shown in FIGURE 8.
- FIGURE 8 a bundle of tube elements of rectangular transverse cross section is positioned inside a casing member 61 with a corresponding transverse cross section.
- the bundle of tube elements shown in FIGURE 8 has been provided with one form of a supporting framework as previously described.
- This tube bundle is mounted in position at each end of the casing member 61 by means of split plates 65 which engage flange 62 around the end opening of the casing member 61 and fit closely around and engages one side of the flange member 59 around the end of the tube bundle.
- Each end of the casing member 61 is provided with a header member 64 with flange 63.
- the header member When the header member is assembled its flange 63 is fitted closely around the end of the tube bundle and engages the other side flange member 59 on the end of the bundle.
- the flanges 62 and 63 When the flanges 62 and 63 are bolted together their clamping engagement with opposite sides of flange 59 forms an end closure for the apparatus and maintains the desired separation of the fluid passing through the tube elements from the fluid passing into the casing member 61 through inlet connection means 163, transversely through casing member 61 across the exteriors of the tube elements, and out of the casing member through outlet connection means 164.
- FIGURE 10 discloses a heat exchange apparatus formed by assembling a plurality of components each of which comprise a transversely extending integral molded structure MS at each end of a single layer warp of tube elements and further comprises a transversely extending integral molded structure MSA formed by physically uniting the tube elements at a position intermediate the ends thereof.
- the molded structures intermediate the ends of the array of tube elements are provided with two opposed major surfaces which are planar and parallel.
- a plurality of components of this type are stacked as shown in FIGURE with alternate components having their integral molded structure MS at their end portions brought together in stacked arrangement, and suitably bonded to each other by adhesives or welding to form an end unit with a transverse cross section suitable for being received in, secured, and sealed in openings 72 in the header members 71 as shown.
- the opposing planar surfaces of the integral molded structures MSA intermediate the ends of the tube elements are maintained in operative heat transfer engagement with each other by means such as gravity or suitable bonding so that heat transfer occurs between a fluid passing through one component and a fluid passing through the adjacent components without the need for a surrounding casing or housing member.
- FIGURE 5 A preferred arrangement for manufacturing components of the invention is shown generally and schematically in FIGURE 5.
- a single layer warp, or array, W of continuous tubular elements T is formed by unwinding them from a reel or drum R or other suitable supply means.
- the tubular elements T are constrained into a side-by-side laterally engaged layer and led through a zone occupied by a means E1, E2 for forming an air-tight enclosure across at least a portion of the warp.
- a heating means 4M and a vacuum means VM are operatively associated with the means E1, E2 for applying heat to a portion of a warp which extends through the air-tight enclosure of means E1, E2 and also applying a reduced pressure externally of the tube elements of the heated portion of the warp in order to physically unite the tubes of the portion and form the transversely extending integral molded structure MS.
- at least one end of the tube elements of the warp are open to the atmosphere in order to develop the desired pressure differential across the heated portion of the tubes in the air-tight enclosure.
- the application of heat and differential pressure is terminated and the molded structure MS of the united warp is removed from enclosure means E1, E2 to a position at which the molded structure MS is engaged by a severing means I M to sever the molded structure transversely as indicated in FIG- URE 5 to form the component of the invention indicated by the reference characters HXC.
- the operation is repeated to produce the desired number of components.
- tubular elements are made and the preferred sizes of these elements are disclosed in the above-mentioned U.S. Patent 3,228,456.
- the composition most preferred is a polyfiuorinated plastic such as a copolymer of tetrafluorethylene and hexafluoropropylene.
- the tubular elements in the bundle preferably are in a size range between about 5 and about 275 mils outside diameter with a wall thickness between about 0.5 and about 30.0 mils. Such tubular elements are usually quite flexible, especially at elevated operating temperatures.
- the preferred fluorinated plastic materials may also conveniently be used to form other elements of the apparatus in addition to the tubular elements; for example, the peripheral flange 59 surrounding the bonded molded structures of the united components of FIGURE 7, and the tubular header members as shown in FIG- URES 6 and 10.
- These materials may be joined to each other conveniently by welding or heat bonding techniques in which the heat-softened or molten parts to be joined are held in engagement under suitable pressure, and allowed to cool in united condition.
- Techniques and arrangements are also known for operatively uniting plastic components as used in this invention with components of other materials such as metals.
- FIGURES 1A and 1B The details of one form of the means E1, E2 which forms the air-tight enclosure around at least a portion of the flat array of tube elements are shown in FIGURES 1A and 1B,
- This means comprises an upper assembly 20 and a lower assembly 40 which are mounted for movement relative to each other between a first position in which the two assemblies engage each other and an array of tube elements to form the air-tight enclosure around at least a portio nof the array, and a second position in which the two assemblies are spaced apart for removal of the united array and entry of a new array for treatment.
- a suitable actuating means AM1 for effecting this relative movement is shown schematically in FIGURE 5, and could be any of many conventional pneumatic, hydraulic, electrical, or mechanical actuating mechanisms.
- a suitable vacuum-producing means VM such as pump is operatively connected to the enclosure-forming means E1, E2 as shown in FIGURE 5.
- Suitable means HM for heating the portion of an array of tube elements contained in the enclosure is also operatively associated with the enclosure and could be any suitable conventional heating arrangement such as electrical or circulating fluid or other type.
- each assembly 20, 40 comprises a main block or structural unit 21, 41 in which are provided suitable passageways for applying the vacuum or reduced pressure to the exterior of tube elements of a warp portion enclosed by said assemblies.
- suitable passageways for applying the vacuum or reduced pressure to the exterior of tube elements of a warp portion enclosed by said assemblies.
- two opposed surfaces for applying a clamping force to the tube element of an enclosed warp tending to flatten the tube elements and move the engaged portions of the tube elements into firm lateral engagement
- warp heating means cooperating with said opposed surfaces are provided in these assemblies.
- the vacuum passageways comprise two elongated transversely extending cylindrical passageways 47 extending across the unit 41, each passageway communicating with a parallel groove 49 through a number of short passageways 48 spaced along the length of the groove and the elongated passageways.
- Passageways 47 are adapted by conventional means to be operatively connected to a vacuum pump or other pressure reducing means by suitable conduits and connections not shown.
- a flat surface 43 is provided in unit or block 41. This surface corresponds to a similar opposed surface 23 in unit or block 21 so that when the two assemblies are positioned in engagement about a layer or warp of tube elements, these surfaces carry out the above-mentioned clamping action on the engaged elements.
- FIGURE 4 illustrates the lower assembly 40 in a plan view with a warp or array of tube elements positioned therein prior to engagement with the upper assembly 20.
- two parallel transversely extending recesses 44 are shown with openings 46 at the side of the unit.
- Lower unit 41 is provided with opposed side walls 51 each having a portion 42 extending therefrom. These side walls define a space for receiving an array or warp of tube elements as shown in FIGURE 4, and cooperate with corresponding side walls on the upper unit 21 to form the air-tight enclosure around a warp when the two units are brought together into engagement with each other and the warp. It will be clear from FIGURES 1A and 1B that the upper unit 21 is similar in features and function to lower unit 41 just described.
- FIGURE 4 illustrates the clamping action of the opposed surfaces OS (43, 23, of units 41, 21) on the tubes of a warp engaged between assemblies and 40.
- Units 21 and 41 are preferably made of a strong insulating thermoset plastic material except for the opposed clamping surfaces which preferably are formed of metal in order to perform their heat transfer function effectively.
- an array of tube elements with at least one end of each of the tube elements open to atmospheric pressure is placed in position on lower unit 41 as shown in FIGURE 4, and the upper and lower units are brought together into engagement with each other and the array to form the air-tight enclosure about the engaged portion of the warp.
- the pressure is then reduced inside the enclosure and exteriorly of the tube elements by means of passageways 47, 48, 27, 28; grooves 29, 49; and vacuum means VM while the portions of the elements engaged by the opposed clamping surfaces 23, 43 are being heated by heater units 45, 25.
- FIGURE 3 After which the heat and pressure differential are terminated, the structure allowed to cool, the assemblies 20, 40 moved to their spaced apart positions, and the structure removed therefrom.
- a vacuum of 12 to 18 inches of water and heating the tube elements to about 285 C. are sufficient to form satisfactory molded structures. It is possible to remove such structures from the assemblies 20, 40 after they have cooled to about 250 C. in order to shorten the cycle of operation.
- a stronger more rigid molded structure can be formed if a transversely extending flat strip of material of the same or similar composition as the tube elements is placed between each of the opposed surfaces 23, 43 and the tube array in an arrangement similar to that of FIGURE 2 where the elements indicated at OS would represent the fiat strips. These strips become a part of the integral molded structure MS under the heat and pressure differential applied within the engaged assemblies 20 and 40 during operation.
- the molded structures MS of the components can be joined together to form a tube bundle, one end of one version being shown in FIGURE 7.
- the components are joined together by heating the opposed surfaces to a softened bondable condition and applying pressure to hold and unite the components to each other.
- Another method of joining the molded structures at the ends of stacked or wound components to form a tube element bundle involves the use of a special composite bonding or fusing tape or sheet comprising a thin film of tetrafiuorethylene rendered electrically conductive by having carbon or other conducting particles dispersed therein, this film being positioned between two adherent thin layers of the same material as that forming the tube elements.
- the composite sheet or tape is positioned between opposing surfaces of two molded structures under light pressure and sufficient electric current passed through the composite tape or sheet to cause fusion and bonding of the opposed surfaces to the composite tape and each other. This can be accomplished in stacked arrangements of components similar to that shown in FIGURE 7 and in wound arrangements similar to that shown in FIGURE 11.
- FIGURE 11 schematically represents another version of an arrangement for forming the transversely extended molded structures on a warp of tube elements.
- the molded structure is progressively formed, either in steps or continuously, transversely across a single layer warp of tube elements.
- Air-tight enclosure means E1, E2 operate at each end of the warp and if desired, one or more of these means could operate to form molded structures at positions intermediate the ends as shown.
- the component formed by this arrangement would be of indefinite width or transverse dimension, and could be used to form composite tube element bundles for heat exchange units either by (l) severing the united warp along a line parallel to the tube elements, stacking, and bonding such severed components to form thet bundle; or (2) winding up and bonding the single component of indefinite length as illustrated in FIGURE 11.
- the bonding means BM is shown at each end of the warp being wound and heats the transversely extending molded structure surfaces so that they will fuse together under the pressure in the Wound unit. The heating accomplished by the means BM also causes the structures MS to be more easily wound up due to their softened condition.
- the staggered short length molded structures intermediate the ends of the bundle can be used to help stabilize the bundle configuration and, if desired, act as baflie arrangements in certain installations.
- FIGURES 12 and 13 illustrate other forms that a wound-up bundle might take, depending on the transverse cross section of the wind-up mandrel which may or may not remain in the bundle in its final form.
- an assemblable component suitable for heat exchange comprising a plurality of elongated flexible tubular elements formed of a solid polymeric composition, said elements arranged in a substantially fiat laterally disposed single layer side-by-side array with the elements substantially parallel to each other, said array having a transverse and a longitudinal dimension said tubular elements at one end of said component having their terminal portions physically united to the corresponding terminal portions of the adjacent tubular elements to form a single integral molded structure extending transversely across the array of said tubular elements, said integral molded structure having passageways extending therethrough each communicating with the interior of a hollow tube element at one end of said molded structure, said tubular elements having a substantially circular transverse cross section and being transversely movable relative to each other along their lengths except for said united portions, the passageways in said integral molded structure having a generally uniform transverse cross sections in the form of a four sided figure comprising two opposed substantially parallel generally planar walls connected by tWo opposed equidistant walls
- the component of claim 1 which further comprises a relatively rigid supporting framework structure engaging the freely transversely movable portions of said tubular elements to maintain said elements in a predetermined configuration and position.
- said framework structure comprises a plurality of elongated members extending transversely of and interengaged with the tubular elements of said array at spaced positions along said array, said elongated members connected at the end portions to laterally spaced elongated members extending longitudinally along said tubular elements.
- An improved heat exchange unit comprising in combination a first header member having an opening formed therein, a second header member having an opening formed therein, said unit further comprising at least one single layer warp of elongated flexible tube elements formed of an organic polymeric composition extending between said header members and operatively secured thereto, the, terminal portions of the tube elements at each end of each said warp being physically united to corre sponding terminal portions of the adjacent tube elements to form a single integral molded structure extending transversely of each said warp, said molded structure having passageways extending therethrough each passageway communicating with the interior of a tube element at one end of the molded structure, a portion of the transversely extending molded structure at each end of each said warp having a transverse cross section corresponding to and secured Within the opening in one of said header members, said unit further comprising fluid sealing means cooperating with said portions of said molded structures and said header members to maintain them in fluid tight relationship.
- An improved heat exchange unit comprising in combination a first header member having an axially extending elongated slot formed therein, a second header member having an axially extending elongated slot formed therein, said unit further comprising at least one single layer warp of elongated flexible tube elements formed of an organic polymeric composition extending between said header members and operatively secured thereto, the terminal portions of the tube elements at each end of each said warp being physically united to corresponding terminal portions of the adjacent tube elements to form a single integral molded structure extending transversely of each said warp, said molded structure having passageways extending therethrough each passageway communicating with the interior of a tube element at one end of the molded structure, a portion of the transversely extending molded structure at each end of each said warp having a transverse cross section corresponding to and secured'within the slot in one of said header members, said unit further comprising fluid sealing means cooperating with said portions of said molded structures and said header members to maintain them in fluid tight relationship.
- said framework structure comprises a plurality of elongated members extending transversely of and interengaged with the tubular elements of said array at spaced positions along said array, said elongated members connected at the end portions to laterally spaced elongated members extending longitudinally along said tubular elements.
- header members are elongated tubular members of an organic polymeric composition.
- an assemblable component suitable for fluid handling said component comprising a plurality of elongated flexible tubular elements formed of a solid polymeric composition, said elements arranged in a substantially fiat laterally disposed single layer side-by-side array, said tubular elements at least one portion of said component having their laterally adjacent portions physically united to the corresponding portions of the laterally adjacent tubular elements to form a single integral molded structure extending transversely across the array of said tubular elements, said integral molded structure having passageways extending therethrough each communicating with the interior of a tube element at least one end of said molded structure, said tubular elements having a substantially circular transverse cross section along their length except for said united portions, the passageways in said integral molded structure, each having a generally uniform transverse cross section in the form of a four sided figure comprising two opposed substantially parallel planar walls connected by two opposed equidistant walls, said substantially parallel walls formed by the merging of two engaged walls of the circular cross sectioned tubular elements, said opposed equid
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Description
I April 1, 1969- M. s. WITHERS 3,435,893
HEAT BXCHANGER COMPONENT FORMED WITH FLEXIBLE PLASTIC TUBES Sheet of 5 Filed July, :51, 19s? INVENTOR MICHAEL SOHERVILLE WITHERS law A ATTORNEY April 1, 1969 l M. s. WITHE RS 3,435,893
HEAT EXCHANGER COMPONENT FORMED WITH FLEXIBLE PLASTIC TUBES Filed July 31, 1967 Sheet 2 of 5 40 MICHAEL SOHERVILLE WIYTHERS INVENTOR BY v ATTORNEY HEATEXCHANGERHCOMPONENT FORMED WITH FLEXIBLE PLASTIC TUBES Filed Jul 31, 1967 v April 1, 1969 M. s. WITHERS Sheet 3 of FIE-2.6
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S H I I D I 4 i v [/10 I l I I I l I I I P I H INVENJFOR MICHAEL SOMERVILLE WITHERS ATTORNEY April 1,- 1969 s. WITHERS HEAT EXCHANGER COMPONENT FORMED WITH FLEXIBLE PLASTIC TUBES Filed July 31, 1967 Sheet FIG. 8
INVENTOR MICHAEL SOMERVILLE WITHERS ATTORNEY 1969 M; svQrrHks I 3, '1 I HEAT EXCHANGER COMPONENT FORMED WKTH FLEXIBLE PLASTIC TUBES Filed July :51. 1967 She et ,2 of 5 Fl e."11
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INVENTOR MICHAEL SOMERVILLE WITHERS ATTORNEY United States Patent US. Cl. 165158 13 Claims ABSTRACT OF THE DISCLOSURE An assemblable component suitable for heat exchange, or heat transfer, comprising a plurality of elongated flexible plastic tubular elements arranged in a substantially flat laterally disposed single layer side-by-side array, said tubular elements of at least one portion of the component having their laterally adjacent portions physically united to each other to form a single integral molded structure extending transversely of said array, said molded structure having passageways of a particular transverse crosssection extending therethrough, each communicating with the interior of a tube element at at least one end of the molded structure, the molded structure having a particular configuration to permit stacking or windup to produce multi-layer units. Also involved is an improved manufacturing arrangement for producing the simplified easily assemblable components.
Introduction This invention relates generally to heat exchange, or heat transfer, apparatus; and more specifically to a particular heat exchange apparatus construction formed from flexible plastic tube elements and especially useful in certain applications.
It is an object of the invention to provide a simplified, novel, and improved structure formed of flexible plastic hollow tube elements and suitable for performing a heat transfer function in a heat transfer apparatus or process involving a plurality of fluids. It is an object of the invention to provide such a structure which is simple and economical in its construction, yet effective and reliable in use, such structure also being capable of convenient expeditions fabrication and assembly into composite heat transfer, or heat exchange, apparatus units.
It is a further object to provide such a structure which in its features, its functioning, and its manufacture overcomes certain disadvantages and problems involved in prior art heat exchange structures of the type utilizing flexible plastic tube elements as will be discussed hereinafter.
Other objects and advantages will appear from a consideration of the following specification, claims, and accompanying drawings.
Background of the invention As indicated in US. Patents 3,315,740, 3,228,456, and 3,277,959, heat transfer processes and apparatus utilizing flexible plastic tubular elements are known, and because of the use of this type tubular elements, a number of special problems have been faced in designing, producing, and operating such arrangements.
In one of these arrangements, the flexible plastic tube elements must be individually threaded through baifle members and secured individually in tube sheet members. In other of these arrangements, the tube elements are fashioned into bundles using transverse tapes which must be secured to the tube elements by welding or adhesives. In still other arrangements. (application Ser. No. 598,070, filed Nov. 30, 1966), additional means such as foraminous cylinders, or baskets, are needed in addition to the tapes to maintain the position and size of a \bundle of heat exchange tubes. Bundles of flexible plastic tubes also have been formed by assembling sleeves of braided tubes in order to provide coherent stable bundles (application Ser. No. 634,631, filed Apr. 28, 1967). These previous arrangements are somewhat complex, costly, and involve certain problems in operation and maintenance.
The components of this invention, due to their simplicity, no additional elements being required, in the preferred version, other than the flexible plastic tube elements themselves, and due to the ease of assembly into composite heat exchanger units, presents an improved product over the prior art arrangements and also makes possible the use of more simple and eflicient production techniques. The improved component, due to its novel construction, can be used to produce special configuration heat exchanger units greatly reduced in one of their three dimensions for use in special limited space applications. The elimination of tapes, and braids, and supporting baskets in the preferred embodiments of the invention not only reduces complexity and cost, but also improves fluid flow characteristics by reducing pressure drop and reducing susceptibility to clogging due to foreign matter in the fluid streams being handled exteriorly of the hollowtubular elements.
The improved component when used in a flat warp configuration of the tube elements, or in a rectangular transverse crosssection multi-layer assembly is especially advantageous in heat exchangers of the cross flow type in which one fluid stream is passed substantially perpendicularly, or transversely, across a bundle of tube elements carrying another fluid stream for heat transfer between the streams.
The advantages and features mentioned generally in the preceding paragraphs will be discussed in detail hereinafter.
In the drawings,
FIGURES 1A and 1B are perspective views of the main units of the apparatus for forming the improved component of this invention, by creating a tight enclosure around a warp of tube elements and applying the required heat and reduced pressure to the tube elements to physically unite them.
FIGURE 2 is a partial perspective view of the terminal portions of a single layer parallel array of plastic tube elements positioned between two opposed heated surfaces as would occur in the units of FIGURES 1A and 1B to apply the heat and pressure to physically unite the tube elements to form the component of this invention.
FIGURE 3 is a view similar to FIGURE 2 showing the united tube elements of the component of this invention.
FIGURE 4 is a partial plan view of the apparatus unit of FIGURE 1B showing a warp or array of tube elements positioned therein prior to the uniting operation.
FIGURE 5 is a general schematic showing of one overall arrangement for producing components suitable for heat exchange and embodying principles of the invention.
FIGURE 6 is a perspective exploded view of a simplified heat exchange unit formed using a single component of this invention.
FIGURE 7 is a partial perspective view of one end of a rectangular transverse cross-section heat exchanger unit formed by assembling a plurality of components of this invention.
FIGURE 8 is a partial simplified perspective view of an overall cross flow heat exchanger utilizing a rectangular transverse cross-section assembly of components of this invention with certain parts broken away for a clearer general showing.
FIGURE 9 is a series of schematic views. of components of the invention showing a number of the possible transverse cross-sectional arrangements of the united molded structure which would permit assembly by stacking or winding up of components.
FIGURE is an exploded perspective view of an assembled heat exchange unit utilizing components of this invention Which have the transverse molded or united structure formed not only across the terminal portion of the tube elements to facilitate connection to the header members, but also across intermediate portions of the tube elements to provide for heat transfer between alternate layers of the tube elements without the need for the usual shell or casing.
FIGURE 11 is a generalized schematic showing of another arrangement for producing components embodying principles of this invention and assembling the component into a multilayer bundle.
FIGURES 12 and 13 show multilayer bundles of different transverse cross sections which can be prepared by the arrangement of FIGURE 11.
The basic structure of an assemblable component embodying principles of the invention is shown in FIGURE 3. One version of a complete component embodying features of the invention is shown in FIGURE 6 and identified by the reference character HXCI. Generally, as viewed in FIGURE 3, the component comprises a side- 'by-side single layer array or warp of elongated flexible tube elements T formed of an organic polymeric composition, which tube elements are laterally joined together or physically united in at least one transversely extending integral structure MS. The tube elements are united by any suitable means, preferably a molding arrangement to be described at a later point. This integral structure is provided with elongated passageways P extending therethrough, each passageway communicating with the interior of a hollow tubular element T at at least one end of the integral or molded structure MS. The passageways in the integral structure have generally uniform transverse cross sections. with four sides as shown. The opposed walls 10 which divide the integral structure laterally to form the passageways P are substantially parallel to each other and are generally planar. These Walls 10 are joined or connected as shown in FIGURE 3 by two opposed equidistant walls 11 which are faired together in a lateral direction to form opposing transversely extending regular surfaces constructed and arranged to engage and match with other similar structures of tubular elements, or with other portions of the same structure when folded or wound, so that a heat exchange bundle of a plurality of layers, as shown in FIGURES 7, 8, 10, ll, 12 and 13, can conveniently be assembled and formed. The preferred and simplest arrangement of fairing together the equidistant walls to provide the regular opposed surfaces suitable for forming multi-layer arrangements is the one in which all of the opposed walls on one side of the molded structure are joined to form a single transversely extending planar surface as shown in FIGURE 3. However other arrangements may be formed and used such as those having transverse cross sections as shown in FIGURE 9. The heat exchange bundles are formed by winding or stacking the assemblable components and suitably bonding these components together at least at the end portions where the tube elements are physically united to form the transversely extending integral molded structures.
The component HXCI shown in FIGURE 6 can be provided with a relatively rigid supporting framework, which may be a wire grid interwoven with the tube elements T. As shown the grid comprises transversely extending elements 56 which are interconnected at their end portions by longitudinal elements 55. The supporting framework is used where it is desired to maintain the flexible array of tube elements in a given position and for configuration. Another type of supporting framework is shown in FIGURE 8 in which a tube bundle of rectangular transverse cross section is built up of a plurality of single layer arrays of tube elements or components of the invention. The framework of FIGURE 8 comprises at a number of longitudinally spaced positions along the bundle of tube elements, a plurality of transversely extending members 66 each placed between a layer of tube elements and joined at their ends by elongated bolt members 67. If desired, the transversely extending members 66 may be further secured in place by an adhesive bond to the engaged layers of tube elements.
Another version of the assemblable component of the invention is disclosed in FIGURE 10. These components are identical with the components shown in FIGURES 3 and 6 except that they are further provided intermediate their end portions with an additional transversely extending integral molded structure MSA formed by physically united tube elements for a purpose to be disclosed hereinafter.
The components embodying principles of the invention may be used individually as shown in FIGURE 6 by suitably securing and sealing the transversely extending molded structures MS in openings 52, 54 in header members 51 and 53 respectively. The component of course may be used with and without a supporting framework. Header members 51 and 53 can conveniently be made of an organis polymeric composition compatible with the material of which the tube elements are formed.
The components of the invention may be used in a multilayer stacked arrangement as shown in FIGURES 7 and 8. This arrangement is formed by stacking or superimposing one on the other a plurality of components such as those shown in FIGURES 3 and 6 and sealing or bonding the transversely extending integral molded structures MS to each other at each end of the stacked arrangement. When components of the same length and width are used in such an arrangement, a bundle of tube elements with a rectangular transverse cross section is formed as seen in FIGURE 7. Usually a rigidly secured peripherally surrounding flange member 59 is provided at each end of the bundle to assist in its assembly into a complete heat exchanger apparatus of the type generally shown in FIGURE 8. In FIGURE 8, a bundle of tube elements of rectangular transverse cross section is positioned inside a casing member 61 with a corresponding transverse cross section. The bundle of tube elements shown in FIGURE 8 has been provided with one form of a supporting framework as previously described. This tube bundle is mounted in position at each end of the casing member 61 by means of split plates 65 which engage flange 62 around the end opening of the casing member 61 and fit closely around and engages one side of the flange member 59 around the end of the tube bundle.
Each end of the casing member 61 is provided with a header member 64 with flange 63. When the header member is assembled its flange 63 is fitted closely around the end of the tube bundle and engages the other side flange member 59 on the end of the bundle. When the flanges 62 and 63 are bolted together their clamping engagement with opposite sides of flange 59 forms an end closure for the apparatus and maintains the desired separation of the fluid passing through the tube elements from the fluid passing into the casing member 61 through inlet connection means 163, transversely through casing member 61 across the exteriors of the tube elements, and out of the casing member through outlet connection means 164.
FIGURE 10 discloses a heat exchange apparatus formed by assembling a plurality of components each of which comprise a transversely extending integral molded structure MS at each end of a single layer warp of tube elements and further comprises a transversely extending integral molded structure MSA formed by physically uniting the tube elements at a position intermediate the ends thereof. The molded structures intermediate the ends of the array of tube elements are provided with two opposed major surfaces which are planar and parallel. A plurality of components of this type are stacked as shown in FIGURE with alternate components having their integral molded structure MS at their end portions brought together in stacked arrangement, and suitably bonded to each other by adhesives or welding to form an end unit with a transverse cross section suitable for being received in, secured, and sealed in openings 72 in the header members 71 as shown. The opposing planar surfaces of the integral molded structures MSA intermediate the ends of the tube elements are maintained in operative heat transfer engagement with each other by means such as gravity or suitable bonding so that heat transfer occurs between a fluid passing through one component and a fluid passing through the adjacent components without the need for a surrounding casing or housing member.
The structure and functioning of the components, as well as the operation of the assembled multi-component heat transfer units, or apparatus, is believed to be clear from the preceding description and the accompanying drawings.
A preferred arrangement for manufacturing components of the invention is shown generally and schematically in FIGURE 5. In this arrangement a single layer warp, or array, W of continuous tubular elements T is formed by unwinding them from a reel or drum R or other suitable supply means. The tubular elements T are constrained into a side-by-side laterally engaged layer and led through a zone occupied by a means E1, E2 for forming an air-tight enclosure across at least a portion of the warp. A heating means 4M and a vacuum means VM are operatively associated with the means E1, E2 for applying heat to a portion of a warp which extends through the air-tight enclosure of means E1, E2 and also applying a reduced pressure externally of the tube elements of the heated portion of the warp in order to physically unite the tubes of the portion and form the transversely extending integral molded structure MS. In this arrangements at least one end of the tube elements of the warp are open to the atmosphere in order to develop the desired pressure differential across the heated portion of the tubes in the air-tight enclosure. After the molded structure MS has been formed the application of heat and differential pressure is terminated and the molded structure MS of the united warp is removed from enclosure means E1, E2 to a position at which the molded structure MS is engaged by a severing means I M to sever the molded structure transversely as indicated in FIG- URE 5 to form the component of the invention indicated by the reference characters HXC. The operation is repeated to produce the desired number of components.
The preferred composition of which the tubular elements are made and the preferred sizes of these elements are disclosed in the above-mentioned U.S. Patent 3,228,456. The composition most preferred is a polyfiuorinated plastic such as a copolymer of tetrafluorethylene and hexafluoropropylene. The tubular elements in the bundle preferably are in a size range between about 5 and about 275 mils outside diameter with a wall thickness between about 0.5 and about 30.0 mils. Such tubular elements are usually quite flexible, especially at elevated operating temperatures.
However, it is believed to be clear to those of ordinary skill in the art involved that other materials could be utilized without departing from the spirit of the invention. Many other organic polymeric compositions could be used so long as they were thermoplastic, possessed suitable compatibility with the fluids handled, possessed adequate properties such as strength at the operating conditions of the apparatus, and further possessed adequate thermal conductivity for the intended use.
The preferred fluorinated plastic materials, especially for heat transfer applications involving corrosive fluids, may also conveniently be used to form other elements of the apparatus in addition to the tubular elements; for example, the peripheral flange 59 surrounding the bonded molded structures of the united components of FIGURE 7, and the tubular header members as shown in FIG- URES 6 and 10. These materials may be joined to each other conveniently by welding or heat bonding techniques in which the heat-softened or molten parts to be joined are held in engagement under suitable pressure, and allowed to cool in united condition. Techniques and arrangements are also known for operatively uniting plastic components as used in this invention with components of other materials such as metals. Some illustrative constructions and arrangements of this type are shown in the issued U.S. patents and pending patent applications referred to in the preceding portions of this specification.
The details of one form of the means E1, E2 which forms the air-tight enclosure around at least a portion of the flat array of tube elements are shown in FIGURES 1A and 1B, This means comprises an upper assembly 20 and a lower assembly 40 which are mounted for movement relative to each other between a first position in which the two assemblies engage each other and an array of tube elements to form the air-tight enclosure around at least a portio nof the array, and a second position in which the two assemblies are spaced apart for removal of the united array and entry of a new array for treatment. A suitable actuating means AM1 for effecting this relative movement is shown schematically in FIGURE 5, and could be any of many conventional pneumatic, hydraulic, electrical, or mechanical actuating mechanisms. A suitable vacuum-producing means VM such as pump is operatively connected to the enclosure-forming means E1, E2 as shown in FIGURE 5. Suitable means HM for heating the portion of an array of tube elements contained in the enclosure is also operatively associated with the enclosure and could be any suitable conventional heating arrangement such as electrical or circulating fluid or other type.
Referring again to FIGURES 1A and 1B each assembly 20, 40 comprises a main block or structural unit 21, 41 in which are provided suitable passageways for applying the vacuum or reduced pressure to the exterior of tube elements of a warp portion enclosed by said assemblies. In addition, two opposed surfaces for applying a clamping force to the tube element of an enclosed warp tending to flatten the tube elements and move the engaged portions of the tube elements into firm lateral engagement, and warp heating means cooperating with said opposed surfaces are provided in these assemblies. Specifically, referring to FIGURE 1B, the vacuum passageways comprise two elongated transversely extending cylindrical passageways 47 extending across the unit 41, each passageway communicating with a parallel groove 49 through a number of short passageways 48 spaced along the length of the groove and the elongated passageways. Passageways 47 are adapted by conventional means to be operatively connected to a vacuum pump or other pressure reducing means by suitable conduits and connections not shown. As shown in FIGURE 1B a flat surface 43 is provided in unit or block 41. This surface corresponds to a similar opposed surface 23 in unit or block 21 so that when the two assemblies are positioned in engagement about a layer or warp of tube elements, these surfaces carry out the above-mentioned clamping action on the engaged elements. FIGURE 4 illustrates the lower assembly 40 in a plan view with a warp or array of tube elements positioned therein prior to engagement with the upper assembly 20. In FIGURE 1B two parallel transversely extending recesses 44 are shown with openings 46 at the side of the unit. These recesses are positioned adjacent to surface 43 for controlled distribution of heat to the surface 43 from cartridge type electrical resistance heaters positioned in each recess. These heaters are connected to a suitable source of power and control unit by means of suitable connections not shown. Lower unit 41 is provided with opposed side walls 51 each having a portion 42 extending therefrom. These side walls define a space for receiving an array or warp of tube elements as shown in FIGURE 4, and cooperate with corresponding side walls on the upper unit 21 to form the air-tight enclosure around a warp when the two units are brought together into engagement with each other and the warp. It will be clear from FIGURES 1A and 1B that the upper unit 21 is similar in features and function to lower unit 41 just described. When the units or assemblies are engaged about a portion of a tube array, opposed resilient sealing strips 401 and 201 at each end of the units engage the tube elements to form an air-tight seal about the tube elements. The elements indicated at C in FIGURE 4 are lateral guide or positioning means for constraining a warp of tube elements into a close side-by-side arrangement prior to formation of the transversely extending integral molded structure MS. FIGURE 2 illustrates the clamping action of the opposed surfaces OS (43, 23, of units 41, 21) on the tubes of a warp engaged between assemblies and 40. Units 21 and 41 are preferably made of a strong insulating thermoset plastic material except for the opposed clamping surfaces which preferably are formed of metal in order to perform their heat transfer function effectively.
In operation, an array of tube elements with at least one end of each of the tube elements open to atmospheric pressure is placed in position on lower unit 41 as shown in FIGURE 4, and the upper and lower units are brought together into engagement with each other and the array to form the air-tight enclosure about the engaged portion of the warp. The pressure is then reduced inside the enclosure and exteriorly of the tube elements by means of passageways 47, 48, 27, 28; grooves 29, 49; and vacuum means VM while the portions of the elements engaged by the opposed clamping surfaces 23, 43 are being heated by heater units 45, 25. When the required combination of heat and pressure differential across the tube element walls is reached the tube elements between the clamping surfaces 23, 43 are united and molded to form the transversely extending integral structure MS is shown in FIGURE 3, after which the heat and pressure differential are terminated, the structure allowed to cool, the assemblies 20, 40 moved to their spaced apart positions, and the structure removed therefrom. With the preferred tube element material (copolymer of TFE and HEP) and tube element dimensions of 80 mils outside diameter and 8 mils wall thickness, a vacuum of 12 to 18 inches of water and heating the tube elements to about 285 C. are sufficient to form satisfactory molded structures. It is possible to remove such structures from the assemblies 20, 40 after they have cooled to about 250 C. in order to shorten the cycle of operation.
If desired, a stronger more rigid molded structure can be formed if a transversely extending flat strip of material of the same or similar composition as the tube elements is placed between each of the opposed surfaces 23, 43 and the tube array in an arrangement similar to that of FIGURE 2 where the elements indicated at OS would represent the fiat strips. These strips become a part of the integral molded structure MS under the heat and pressure differential applied within the engaged assemblies 20 and 40 during operation.
The molded structures MS of the components can be joined together to form a tube bundle, one end of one version being shown in FIGURE 7. The components are joined together by heating the opposed surfaces to a softened bondable condition and applying pressure to hold and unite the components to each other. Another method of joining the molded structures at the ends of stacked or wound components to form a tube element bundle involves the use of a special composite bonding or fusing tape or sheet comprising a thin film of tetrafiuorethylene rendered electrically conductive by having carbon or other conducting particles dispersed therein, this film being positioned between two adherent thin layers of the same material as that forming the tube elements. The composite sheet or tape is positioned between opposing surfaces of two molded structures under light pressure and sufficient electric current passed through the composite tape or sheet to cause fusion and bonding of the opposed surfaces to the composite tape and each other. This can be accomplished in stacked arrangements of components similar to that shown in FIGURE 7 and in wound arrangements similar to that shown in FIGURE 11.
FIGURE 11 schematically represents another version of an arrangement for forming the transversely extended molded structures on a warp of tube elements. In this version, the molded structure is progressively formed, either in steps or continuously, transversely across a single layer warp of tube elements. Air-tight enclosure means E1, E2 operate at each end of the warp and if desired, one or more of these means could operate to form molded structures at positions intermediate the ends as shown. The component formed by this arrangement would be of indefinite width or transverse dimension, and could be used to form composite tube element bundles for heat exchange units either by (l) severing the united warp along a line parallel to the tube elements, stacking, and bonding such severed components to form thet bundle; or (2) winding up and bonding the single component of indefinite length as illustrated in FIGURE 11. In FIGURE 11 the bonding means BM is shown at each end of the warp being wound and heats the transversely extending molded structure surfaces so that they will fuse together under the pressure in the Wound unit. The heating accomplished by the means BM also causes the structures MS to be more easily wound up due to their softened condition. Considerable care must be taken to control the dimensions of the molded structure MS relative to the dimensions of the tube elements in order to ensure Winding up the final bundle in a uniform manner. In FIGURE 11 the staggered short length molded structures intermediate the ends of the bundle can be used to help stabilize the bundle configuration and, if desired, act as baflie arrangements in certain installations.
FIGURES 12 and 13 illustrate other forms that a wound-up bundle might take, depending on the transverse cross section of the wind-up mandrel which may or may not remain in the bundle in its final form.
It is believed to be clear that applicant has provided a novel and improved component for heat transfer in accordance with the objects of the invention. A need has been established, both in new design equipment and in modifications of conventional heat transfer apparatus, for special configuration components greatly reduced in one of their three dimensions. An example of this, in addition to those already disclosed, occurs where it is desired to position new heat transfer components or tube bundles between banks of existing tubes to increase heat transfer capabilities. Another end use particularly fitted to the single layer components of this invention is the tracing of conduits and tanks with flexible bundles of indefinite length.
Although preferred embodiments of the invention have been described in detail in accordance with the patent statutes, many other modifications and variations within the spirit of the invention will occur to those skilled in this art and all such art are considered to fall within the terms of the following claims.
What is claimed is:
1. As an article of manufacture an assemblable component suitable for heat exchange said component comprising a plurality of elongated flexible tubular elements formed of a solid polymeric composition, said elements arranged in a substantially fiat laterally disposed single layer side-by-side array with the elements substantially parallel to each other, said array having a transverse and a longitudinal dimension said tubular elements at one end of said component having their terminal portions physically united to the corresponding terminal portions of the adjacent tubular elements to form a single integral molded structure extending transversely across the array of said tubular elements, said integral molded structure having passageways extending therethrough each communicating with the interior of a hollow tube element at one end of said molded structure, said tubular elements having a substantially circular transverse cross section and being transversely movable relative to each other along their lengths except for said united portions, the passageways in said integral molded structure having a generally uniform transverse cross sections in the form of a four sided figure comprising two opposed substantially parallel generally planar walls connected by tWo opposed equidistant walls, said substantially parallel walls formed by the merging of two adjacent engaged walls of the circular cross sectioned tubular elements, said opposed equidistant walls being faired together in a lateral direction to form opposing transversely extending unbroken regular surfaces of said single integral molded structure, said opposing transversely extending unbroken regular surfaces constructed and arranged to engage with and match closely with other similar structures of tubular elements so that a heat exchange bundle of a plurality of layers can conveniently be assembled and formed.
2. The component of claim 1 which further comprises a relatively rigid supporting framework structure engaging the freely transversely movable portions of said tubular elements to maintain said elements in a predetermined configuration and position.
3. The component of claim 2 in which said framework structure comprises a plurality of elongated members extending transversely of and interengaged with the tubular elements of said array at spaced positions along said array, said elongated members connected at the end portions to laterally spaced elongated members extending longitudinally along said tubular elements.
4. The component of claim 3 in which said framework structure comprises a rectangular wire grid interwoven with said tubular elements.
5. An improved heat exchange unit comprising in combination a first header member having an opening formed therein, a second header member having an opening formed therein, said unit further comprising at least one single layer warp of elongated flexible tube elements formed of an organic polymeric composition extending between said header members and operatively secured thereto, the, terminal portions of the tube elements at each end of each said warp being physically united to corre sponding terminal portions of the adjacent tube elements to form a single integral molded structure extending transversely of each said warp, said molded structure having passageways extending therethrough each passageway communicating with the interior of a tube element at one end of the molded structure, a portion of the transversely extending molded structure at each end of each said warp having a transverse cross section corresponding to and secured Within the opening in one of said header members, said unit further comprising fluid sealing means cooperating with said portions of said molded structures and said header members to maintain them in fluid tight relationship.
6. An improved heat exchange unit comprising in combination a first header member having an axially extending elongated slot formed therein, a second header member having an axially extending elongated slot formed therein, said unit further comprising at least one single layer warp of elongated flexible tube elements formed of an organic polymeric composition extending between said header members and operatively secured thereto, the terminal portions of the tube elements at each end of each said warp being physically united to corresponding terminal portions of the adjacent tube elements to form a single integral molded structure extending transversely of each said warp, said molded structure having passageways extending therethrough each passageway communicating with the interior of a tube element at one end of the molded structure, a portion of the transversely extending molded structure at each end of each said warp having a transverse cross section corresponding to and secured'within the slot in one of said header members, said unit further comprising fluid sealing means cooperating with said portions of said molded structures and said header members to maintain them in fluid tight relationship.
7. The unit of claim 6 in which said tubular elements are freely transversely movable relative to each other at portions intermediate said terminal portions, and which unit further comprises a relatively rigid supporting framework structure engaging the freely transversely movable portions of said tubular elements to maintain said elements in a predetermined configuration and position.
8. The unit of claim 7 in which said framework structure comprises a plurality of elongated members extending transversely of and interengaged with the tubular elements of said array at spaced positions along said array, said elongated members connected at the end portions to laterally spaced elongated members extending longitudinally along said tubular elements.
9. The unit of claim 8 in which said framework structure comprises a rectangular wire grid interwoven with said tubular elements.
10. The unit of claim 6 in which said header members are elongated tubular members of an organic polymeric composition.
11. The improved unit of claim 5 in which portions of the tube elements of each said warp, at a position intermediate the ends thereof, are physically united to portions of adjacent tube elements to form a single integral molded structure extending transversely of each said warp, said molded structure having passageways extending therethrough, each passageway communicating with the interior of a tube element at each end of the molded structure, the passageways in the molded structure having generally uniform transverse cross sections in the form of a four sided figure having two opposed substantially parallel generally planar walls connected by two opposed equidistant walls, said substantially parallel walls formed by the merging of two engaged adjacent walls of the tubular elements, said opposed equidistant walls being faired together in a lateral direction to form opposing transversely extending unbroken regular surfaces of said molded structure, said opposing transversely extending unbroken regular surfaces constructed and arranged to engage with and match closely with other similar corresponding structures of tubes so that said molded structures can conveniently be assembled to form a multi-layer assembly.
12. As an article of manufacture an assemblable component suitable for fluid handling said component comprising a plurality of elongated flexible tubular elements formed of a solid polymeric composition, said elements arranged in a substantially fiat laterally disposed single layer side-by-side array, said tubular elements at least one portion of said component having their laterally adjacent portions physically united to the corresponding portions of the laterally adjacent tubular elements to form a single integral molded structure extending transversely across the array of said tubular elements, said integral molded structure having passageways extending therethrough each communicating with the interior of a tube element at least one end of said molded structure, said tubular elements having a substantially circular transverse cross section along their length except for said united portions, the passageways in said integral molded structure, each having a generally uniform transverse cross section in the form of a four sided figure comprising two opposed substantially parallel planar walls connected by two opposed equidistant walls, said substantially parallel walls formed by the merging of two engaged walls of the circular cross sectioned tubular elements, said opposed equidistant walls being faired together in a lateral direction to form opposing transversely extending unbroken regular surfaces of said single integral molded structure, said opposing transversely extending unbroken regular surfaces constructed and arranged to engage with and match closely with other integral structures of tubular elements so that a fluid handling assembly of a plurality of layers can convenient- 1y be assembled and formed.
13. The improved component of claim 12 in which said molded structure is sufficiently deformable to be wound and folded about a line substantially parallel to said tube elements to provide multilayer assemblies.
References Cited UNITED STATES PATENTS 12/1947 Cornelius 29-l57.3 X 1/1953 Pugh 138115 7/1957 Nelson 285137 X 12/1965 Rosman 285-137 X 3/1966 Meagher 16546 ROBERT A. OLEARY, Primary Examiner. ALBERT W. DAVIS, Assistant Examiner.
US. Cl. X.R.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US65738067A | 1967-07-31 | 1967-07-31 |
Publications (1)
Publication Number | Publication Date |
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US3435893A true US3435893A (en) | 1969-04-01 |
Family
ID=24636920
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US3435893D Expired - Lifetime US3435893A (en) | 1967-07-31 | 1967-07-31 | Heat exchanger component formed with flexible plastic tubes |
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Cited By (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3490523A (en) * | 1968-04-08 | 1970-01-20 | Us Health Education & Welfare | Transfer device |
US3652365A (en) * | 1970-01-02 | 1972-03-28 | William C Mallonee | Gas injection apparatus |
US3861162A (en) * | 1973-03-16 | 1975-01-21 | Refrigerated Sea Water Inc | Cooling system and heat transfer assembly |
US3877244A (en) * | 1973-06-11 | 1975-04-15 | Peri Leonard J Di | Modular dry-air evaporative cooler |
US3889744A (en) * | 1972-04-20 | 1975-06-17 | Owens Illinois Inc | Recuperator structures and method of making same |
US3962766A (en) * | 1973-06-08 | 1976-06-15 | Pont-A-Mousson S.A. | Process for assembling tubes of plastics material and assemblies resulting from said process |
FR2428224A2 (en) * | 1978-06-06 | 1980-01-04 | Martel Catala & Cie Ets | Tube bundle for heat exchanger - comprises woven structure contg. weft tubes, weft wires and warp wires, useful esp. as solar energy absorber |
EP0010817A1 (en) * | 1978-11-06 | 1980-05-14 | Akzo N.V. | Apparatus for the exchange of heat by means of channels having a small diameter, and the use of this apparatus in different heating systems |
US4206806A (en) * | 1976-03-15 | 1980-06-10 | Akira Togashi | Heat-conducting oval pipes in heat exchangers |
US4256178A (en) * | 1977-02-17 | 1981-03-17 | Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft | Coaxial heat exchanger and method for constructing a heat exchanger |
EP0086268A1 (en) * | 1982-02-17 | 1983-08-24 | Akzo GmbH | Apparatus in which heat is transmitted through hollow fibres |
US4411310A (en) * | 1978-04-07 | 1983-10-25 | The Boeing Company | Heat exchange apparatus having thin film flexible sheets |
US4432409A (en) * | 1981-11-03 | 1984-02-21 | Northern Solar Systems, Inc. | Rotary heat regenerator wheel and method of manufacture thereof |
US4588543A (en) * | 1982-09-13 | 1986-05-13 | Plascore, Inc. | Method of constructing heat exchanger core |
US4643244A (en) * | 1984-11-07 | 1987-02-17 | E. I. Du Pont De Nemours And Company | Gas-liquid heat exchange process and apparatus |
USRE32461E (en) * | 1973-06-11 | 1987-07-21 | Modular dry-air evaporative cooler | |
US4735261A (en) * | 1982-09-13 | 1988-04-05 | Plascore, Inc. | Plastic heat exchanger |
US4820468A (en) * | 1985-03-22 | 1989-04-11 | Hartig Martval J | Method for making welded hollow plastic plate heat exchangers |
US4834930A (en) * | 1986-04-28 | 1989-05-30 | Akzo N.V. | Method for the manufacture of apparatus for the transfer of heat and/or mass |
EP0331067A2 (en) * | 1988-03-02 | 1989-09-06 | Akzo N.V. | Mass and/or heat exchange apparatus |
US4867233A (en) * | 1986-04-28 | 1989-09-19 | Akzo N.V. | Heat exchanger and method of making heat exchangers |
US4976910A (en) * | 1987-11-30 | 1990-12-11 | Richard Gatley | Method of making a cooling device |
US6660198B1 (en) * | 2000-09-19 | 2003-12-09 | Marconi Communications, Inc. | Process for making a plastic counterflow heat exchanger |
US20080058440A1 (en) * | 2004-07-05 | 2008-03-06 | Siemens Water Technologies Corp. | Hydrophilic Membranes |
US20100000942A1 (en) * | 2006-07-14 | 2010-01-07 | Heinz Joachim Muller | Monopersulfate treatment of membranes |
US20100186927A1 (en) * | 2006-05-04 | 2010-07-29 | John Gietzen | Thermal energy exchanger |
US20100269343A1 (en) * | 2007-04-05 | 2010-10-28 | Greenward Alternatives Llc | Method for Manufacture of Integrated Ridge Vent and Heat Exchanger |
US20110147308A1 (en) * | 2009-12-21 | 2011-06-23 | Siemens Water Technologies Corp. | Charged Porous Polymeric Membranes and Their Preparation |
DE102010024298A1 (en) * | 2010-06-18 | 2011-12-22 | Benteler Automobiltechnik Gmbh | Motor vehicle heat exchanger has heat exchanger cassette and heat exchanger housing, where heat exchanger cassette has multiple heat exchanger plates that are stacked on each other |
US8262778B2 (en) | 2003-07-08 | 2012-09-11 | Siemens Industry, Inc. | Membrane post treatment |
US9453604B1 (en) * | 2012-09-14 | 2016-09-27 | Hrl Laboratories, Llc | Hollow porous materials with architected fluid interfaces for reduced overall pressure loss |
US9783324B2 (en) | 2014-08-26 | 2017-10-10 | The Boeing Company | Vessel insulation assembly |
US9868834B2 (en) | 2012-09-14 | 2018-01-16 | Evoqua Water Technologies Llc | Polymer blend for membranes |
US10179428B2 (en) | 2016-11-17 | 2019-01-15 | The Boeing Company | Mechanically reinforced foam insulation panel and methods of making the same |
US10322375B2 (en) | 2015-07-14 | 2019-06-18 | Evoqua Water Technologies Llc | Aeration device for filtration system |
US10393444B2 (en) | 2013-03-05 | 2019-08-27 | The Boeing Company | Aircraft heat exchanger |
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US2624366A (en) * | 1952-07-22 | 1953-01-06 | William J Pugh | Plural hose |
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Cited By (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3490523A (en) * | 1968-04-08 | 1970-01-20 | Us Health Education & Welfare | Transfer device |
US3652365A (en) * | 1970-01-02 | 1972-03-28 | William C Mallonee | Gas injection apparatus |
US3889744A (en) * | 1972-04-20 | 1975-06-17 | Owens Illinois Inc | Recuperator structures and method of making same |
US3861162A (en) * | 1973-03-16 | 1975-01-21 | Refrigerated Sea Water Inc | Cooling system and heat transfer assembly |
US3962766A (en) * | 1973-06-08 | 1976-06-15 | Pont-A-Mousson S.A. | Process for assembling tubes of plastics material and assemblies resulting from said process |
US3877244A (en) * | 1973-06-11 | 1975-04-15 | Peri Leonard J Di | Modular dry-air evaporative cooler |
USRE32461E (en) * | 1973-06-11 | 1987-07-21 | Modular dry-air evaporative cooler | |
US4206806A (en) * | 1976-03-15 | 1980-06-10 | Akira Togashi | Heat-conducting oval pipes in heat exchangers |
US4256178A (en) * | 1977-02-17 | 1981-03-17 | Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft | Coaxial heat exchanger and method for constructing a heat exchanger |
US4411310A (en) * | 1978-04-07 | 1983-10-25 | The Boeing Company | Heat exchange apparatus having thin film flexible sheets |
FR2428224A2 (en) * | 1978-06-06 | 1980-01-04 | Martel Catala & Cie Ets | Tube bundle for heat exchanger - comprises woven structure contg. weft tubes, weft wires and warp wires, useful esp. as solar energy absorber |
EP0010817A1 (en) * | 1978-11-06 | 1980-05-14 | Akzo N.V. | Apparatus for the exchange of heat by means of channels having a small diameter, and the use of this apparatus in different heating systems |
US4432409A (en) * | 1981-11-03 | 1984-02-21 | Northern Solar Systems, Inc. | Rotary heat regenerator wheel and method of manufacture thereof |
EP0086268A1 (en) * | 1982-02-17 | 1983-08-24 | Akzo GmbH | Apparatus in which heat is transmitted through hollow fibres |
US4588543A (en) * | 1982-09-13 | 1986-05-13 | Plascore, Inc. | Method of constructing heat exchanger core |
US4735261A (en) * | 1982-09-13 | 1988-04-05 | Plascore, Inc. | Plastic heat exchanger |
US4643244A (en) * | 1984-11-07 | 1987-02-17 | E. I. Du Pont De Nemours And Company | Gas-liquid heat exchange process and apparatus |
US4820468A (en) * | 1985-03-22 | 1989-04-11 | Hartig Martval J | Method for making welded hollow plastic plate heat exchangers |
US4867233A (en) * | 1986-04-28 | 1989-09-19 | Akzo N.V. | Heat exchanger and method of making heat exchangers |
US4834930A (en) * | 1986-04-28 | 1989-05-30 | Akzo N.V. | Method for the manufacture of apparatus for the transfer of heat and/or mass |
US4976910A (en) * | 1987-11-30 | 1990-12-11 | Richard Gatley | Method of making a cooling device |
EP0331067A2 (en) * | 1988-03-02 | 1989-09-06 | Akzo N.V. | Mass and/or heat exchange apparatus |
EP0331067A3 (en) * | 1988-03-02 | 1990-01-24 | Akzo N.V. | Mass and/or heat exchange apparatus |
US6660198B1 (en) * | 2000-09-19 | 2003-12-09 | Marconi Communications, Inc. | Process for making a plastic counterflow heat exchanger |
US8262778B2 (en) | 2003-07-08 | 2012-09-11 | Siemens Industry, Inc. | Membrane post treatment |
US20080058440A1 (en) * | 2004-07-05 | 2008-03-06 | Siemens Water Technologies Corp. | Hydrophilic Membranes |
US8524794B2 (en) | 2004-07-05 | 2013-09-03 | Siemens Industry, Inc. | Hydrophilic membranes |
US20100186927A1 (en) * | 2006-05-04 | 2010-07-29 | John Gietzen | Thermal energy exchanger |
US8256497B2 (en) | 2006-05-04 | 2012-09-04 | John Gietzen | Thermal energy exchanger |
US20100000942A1 (en) * | 2006-07-14 | 2010-01-07 | Heinz Joachim Muller | Monopersulfate treatment of membranes |
US20100269343A1 (en) * | 2007-04-05 | 2010-10-28 | Greenward Alternatives Llc | Method for Manufacture of Integrated Ridge Vent and Heat Exchanger |
US20110147308A1 (en) * | 2009-12-21 | 2011-06-23 | Siemens Water Technologies Corp. | Charged Porous Polymeric Membranes and Their Preparation |
DE102010024298A1 (en) * | 2010-06-18 | 2011-12-22 | Benteler Automobiltechnik Gmbh | Motor vehicle heat exchanger has heat exchanger cassette and heat exchanger housing, where heat exchanger cassette has multiple heat exchanger plates that are stacked on each other |
US9453604B1 (en) * | 2012-09-14 | 2016-09-27 | Hrl Laboratories, Llc | Hollow porous materials with architected fluid interfaces for reduced overall pressure loss |
US9862151B1 (en) | 2012-09-14 | 2018-01-09 | Hrl Laboratories, Llc | Hollow porous materials with architected fluid interfaces for reduced overall pressure loss |
US9868834B2 (en) | 2012-09-14 | 2018-01-16 | Evoqua Water Technologies Llc | Polymer blend for membranes |
US10393444B2 (en) | 2013-03-05 | 2019-08-27 | The Boeing Company | Aircraft heat exchanger |
US9783324B2 (en) | 2014-08-26 | 2017-10-10 | The Boeing Company | Vessel insulation assembly |
US10322375B2 (en) | 2015-07-14 | 2019-06-18 | Evoqua Water Technologies Llc | Aeration device for filtration system |
US10179428B2 (en) | 2016-11-17 | 2019-01-15 | The Boeing Company | Mechanically reinforced foam insulation panel and methods of making the same |
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